Optimum Gurney flap height determination for “lost-lift” recovery in compressible dynamic stall control-Reference-Cited by-同舟云学术

Optimum Gurney flap height determination for “lost-lift” recovery in compressible dynamic stall control

Published:2010-12 Issue:8 Volume:14 Page:551-556
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Chandrasekhara M.S.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

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4. M.S. Chandrasekhara, An exploratory investigation of pulsatile blowing to control compressible dynamic stall over an oscillating NACA 0012 airfoil, ARO-STIR Final Report, 2001.

5. Compressible dynamic stall control using a variable droop leading edge airfoil;Chandrasekhara;AIAA J.,2004

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